Hybrid Simulation for Electrically Large Antenna Platforms
Transcript of Hybrid Simulation for Electrically Large Antenna Platforms
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Hybrid Simulation for Electrically Large Antenna Platforms Jim Creed 2016-04-12
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Outline
Introduction to hybrid simulation
Selected antenna platform examples
Conclusions
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The problem…
1.6 GHz
4.5 m
24 λ
1.1 GHz
160 m
560 λ
features:
1 mm
features:
0.5 mm
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CST MWS solver choice
A Range of Solvers…
Ray Tracing
Volumetric Mesh Surface Mesh
Full Wave
Time Domain
FIT, TLM Hexahedral Mesh Conformal (PBA)
Frequency Domain
FEM Tetrahedral Mesh
Curved
Integral Equation
MOM, MLFMM Surface Mesh
Curved
Asymptotic Solver
SBR Surface Mesh
Curved
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Platform Electrical Size
El. Length
1λ
10λ
100λ
1000λ
10000λ
MoM MLFMM
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1. Installed Antenna Scenario
2 GHz
17.4 x 4.5 x 16.2 m
116 x 30 x 108 λ
375,840 λ3
2 GHz blade antenna positioned on aircraft
660 million cells
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1. "Brute Force" Simulation
Single workstation with 2 Kx80
Total memory: < 100 GB
Broadband calculation time ~ few hours
660 million cells
2 GHz blade antenna positioned on aircraft
2 GHz
17.4 x 4.5 x 16.2 m
116 x 30 x 108 λ
375,840 λ3
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2. What if the challenge increases?
aircraft length = 42.6 m
(>2000 λ @ 14.5 GHz)
array(s): 100s of elements element: fine geometry
via radius = 0.4 mm
Several hundred billion cells
Impossible to simulate using only one solver!
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Hybrid: SMALL BIG
near field source
(equivalence principle)
farfield source
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CST MWS Solver ̎ Coupling ̎
1. Combination of different solvers. Coupling
via field
interfaces
2. Loop over the same solver.
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Antenna
choice/synthesis
Of interest:
Antenna Specifications Operating frequency
Farfield
…
Suitable topologies
Antenna
placement
Of interest:
Installed farfield
Coupling with other
antennas
Nearfield calculation
Antenna Placement Workflow
Antenna
simulation
Of interest:
Integration with
other antennas
Matching circuit
Radome
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Antenna
choice/synthesis
Antenna
placement
Antenna Placement Workflow
Antenna
simulation
Different tool/solvers available at each stage…
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Outline
Introduction to hybrid simulation
Selected antenna platform examples
Conclusions
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Three Installed Antenna Examples
1. UAV
2. Satellite
3. Aircraft
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Three Installed Antenna Examples
1. UAV
2. Satellite
3. Aircraft
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a) Antenna placement @ lower frequencies
+ Simple antenna topologies (easy to build from scratch).
+ EM problem not electrically large.
b) Antenna placement @ higher frequencies
More complex antenna topologies (more difficult to build
from scratch).
EM problem electrically large.
UAV Possible Scenarios
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a) Lower Frequencies
VHF blade
30-100 MHz
IFF1 monopole
1020-1100 MHz
IFF2 monopole
1020-1100 MHz
Excitation: Lumped ports @ 50 Ohm
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Brodband Analysis using FIT Calculation time ~ 7min
E-Field @ 1.06 GHz (IFF1)
Farfield @ 1.06 GHz (IFF1)
Polar plot with
structure overlay
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Solution 1 (extract representative antennas)
Solution 2 Use antenna measured data (i.e from MVG).
b) Higher Frequencies
Antenna specification Frequency [GHz]
1 TACAN 1.08
2 GPS 1.575
3 Communication 1.8
4 SATCOM (UHF) 2.3
Antennas from 3rd party CAD of the antennas not available!
placement
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A lot of predefined "Aeronautical" antenna specifications.
Specifications can be used to look for suitable antenna topologies
inside Antenna Magus database.
Specification Library
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4 Parametric Antenna Models + UAV 1 TACAN
2 GPS
3 Communication
(1.8 GHz)
4 SATCOM (UHF)
placement
Extra requirements:
Keep geometrical parameters of each single
project.
Place the antennas on predefined
(parametric) positions.
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Schematic
3D Layout
System Assembly and Modelling
3D Layout (aligned antennas using anchor points)
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Setup of Simulation Projects
Brute force approach
Field decomposition approach
MLFMM
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Installed Antennas using SAM FSC
2. Source(s)
1. Platform
(including part of the platform)
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Installed antennas on UAV
4 Sources
Platform
Field sources installed on platform
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Curved Tri+Quad Meshing
Quad Less memory
Curved Higher accuracy
Surface based meshing
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Available outputs
Broadband antenna to antenna coupling
GPS (fs3) SATCOM (fs4)
E-Field @ 2.3 GHz (SATCOM)
E-Field @ 1.575 GHz (GPS)
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Three Installed Antenna examples
1. UAV
2. Satellite
3. Aircraft
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Design Issues Simulation Issues
source: NASA
Coexistence of
multiple antennas
Thermal / Mechanical
issues
Electromagnetic
design
Installed
performance
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Construction of Model
anchor
points
Schematic
3D Layout
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Ku band offset Gregorian reflector (14.6 GHz)
Reflector Installed Performance
filtered to show rays with only 3 reflections
ray visualisation directivity
11 m “wingspan”
535 λ @ 14.6 GHz
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Three Installed Antenna Examples
1. UAV
2. Satellite
3. Aircraft
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Example: Airborne SATCOM
"Earth gravity" by NASA/JPL/University of Texas Center for Space Research. -
http://www.jpl.nasa.gov/news/news.cfm?release=2007-147. Licensed under Public Domain via Commons -
https://commons.wikimedia.org/wiki/F ile:Earth_gravity.png#/media/F ile:Earth_gravity.png
Ku-band SATCOM: linear polarization
Uplink: 14.0 – 14.5 GHz
Downlink: 12.25 – 12.75 GHz
Additional antenna constraints: form factor, mechanical stability,
aerodynamics, weight
Required:
beam steering and
polarization tracking
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Installed Performance of Phased Array
Glass modeled using ̎̎ Thin panel ̎̎ material
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Outline
Introduction to hybrid simulation
Selected aerospace examples
Conclusions
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Decomposition of a big volume into subvolumes : SMALLER (Source) fine features can be accurately simulated (e.g details of radiating source)
SIMPLIFIED (Platform) mesh can be relaxed for the full model containing the imported source (e.g. increase
time step, speed-up method convergence).
Simulate source with appropriate mesh and solver.
Import external (measured) fields.
No knowledge of antenna structure necessary (IP).
Advantages of Hybrid Approach
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Antenna synthesis
Summary Antenna /Array design
Antenna Installed performance
All antenna design stages with the
best solver in one User Interface